View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 22109U 92058B 23275.84219572 .00002928 00000-0 36412-3 0 9995
2 22109 19.7821 99.0679 0035344 345.4014 14.5378 14.75367077649042
| Epoch (UTC): | 02 October 2023 20:12:45 |
| Eccentricity: | 0.0035344 |
| inclination: | 19.7821° |
| perigee height: | 619 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 99.0679° |
| argument of perigee: | 345.4014° |
| revolutions per day: | 14.75367077 |
| mean anomaly at epoch: | 14.5378° |
| orbit number at epoch: | 64904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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